CA2364284A1 - Moteur-fusee - Google Patents

Moteur-fusee Download PDF

Info

Publication number
CA2364284A1
CA2364284A1 CA002364284A CA2364284A CA2364284A1 CA 2364284 A1 CA2364284 A1 CA 2364284A1 CA 002364284 A CA002364284 A CA 002364284A CA 2364284 A CA2364284 A CA 2364284A CA 2364284 A1 CA2364284 A1 CA 2364284A1
Authority
CA
Canada
Prior art keywords
combustion chamber
rotary
fuel
effluent
combustion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002364284A
Other languages
English (en)
Other versions
CA2364284C (fr
Inventor
Richard D. Stephens
Robert S. Thompson, Jr.
Guido J. Defever
John F. Jones
Dean S. Musgrave
Gregg G. Williams
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Williams International Corp
Original Assignee
Williams International Co., L.L.C.
Richard D. Stephens
Robert S. Thompson, Jr.
Guido J. Defever
John F. Jones
Dean S. Musgrave
Gregg G. Williams
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Williams International Co., L.L.C., Richard D. Stephens, Robert S. Thompson, Jr., Guido J. Defever, John F. Jones, Dean S. Musgrave, Gregg G. Williams filed Critical Williams International Co., L.L.C.
Priority to CA002596503A priority Critical patent/CA2596503C/fr
Priority to CA002596260A priority patent/CA2596260C/fr
Publication of CA2364284A1 publication Critical patent/CA2364284A1/fr
Application granted granted Critical
Publication of CA2364284C publication Critical patent/CA2364284C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/66—Combustion or thrust chambers of the rotary type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Testing Of Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Telescopes (AREA)
CA002364284A 1999-03-10 2000-03-10 Moteur-fusee Expired - Fee Related CA2364284C (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CA002596503A CA2596503C (fr) 1999-03-10 2000-03-10 Ensemble rotor
CA002596260A CA2596260C (fr) 1999-03-10 2000-03-10 Systeme de refroidissement de moteur-fusee

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12362199P 1999-03-10 1999-03-10
US60/123,621 1999-03-10
PCT/US2000/006393 WO2000057048A2 (fr) 1999-03-10 2000-03-10 Moteur-fusee

Related Child Applications (2)

Application Number Title Priority Date Filing Date
CA002596503A Division CA2596503C (fr) 1999-03-10 2000-03-10 Ensemble rotor
CA002596260A Division CA2596260C (fr) 1999-03-10 2000-03-10 Systeme de refroidissement de moteur-fusee

Publications (2)

Publication Number Publication Date
CA2364284A1 true CA2364284A1 (fr) 2000-09-28
CA2364284C CA2364284C (fr) 2008-05-06

Family

ID=22409771

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002364284A Expired - Fee Related CA2364284C (fr) 1999-03-10 2000-03-10 Moteur-fusee

Country Status (11)

Country Link
US (3) US6269647B1 (fr)
EP (1) EP1171705B1 (fr)
JP (3) JP4386589B2 (fr)
CN (2) CN1201076C (fr)
AT (1) ATE386203T1 (fr)
AU (1) AU6045800A (fr)
CA (1) CA2364284C (fr)
DE (2) DE60044733D1 (fr)
IL (4) IL145349A0 (fr)
RU (1) RU2243403C2 (fr)
WO (1) WO2000057048A2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113266492A (zh) * 2021-04-16 2021-08-17 北京星际荣耀空间科技股份有限公司 发动机推力室、火箭发动机、液体火箭

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CN102029981B (zh) * 2009-09-29 2014-12-10 李开超 四种机动车用火箭及制动系统
JP5113230B2 (ja) * 2010-01-04 2013-01-09 貴之 伊東 ロケット発電エンジン及びロケット発電ファンエンジン
CN101915182B (zh) * 2010-06-09 2013-05-22 北京航空航天大学 一种固体燃料火箭发动机
CN101956981B (zh) * 2010-07-08 2012-05-23 中国航天科技集团公司第六研究院第十一研究所 一种气液组元高室压大范围变工况燃烧器
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Cited By (2)

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Publication number Priority date Publication date Assignee Title
CN113266492A (zh) * 2021-04-16 2021-08-17 北京星际荣耀空间科技股份有限公司 发动机推力室、火箭发动机、液体火箭
CN113266492B (zh) * 2021-04-16 2022-03-15 北京星际荣耀空间科技股份有限公司 发动机推力室、火箭发动机、液体火箭

Also Published As

Publication number Publication date
CN1670353A (zh) 2005-09-21
DE60044733D1 (de) 2010-09-02
CN1343282A (zh) 2002-04-03
IL164183A0 (en) 2005-12-18
EP1171705A2 (fr) 2002-01-16
IL145349A (en) 2007-06-17
JP2002540340A (ja) 2002-11-26
ATE386203T1 (de) 2008-03-15
US6205770B1 (en) 2001-03-27
JP4386589B2 (ja) 2009-12-16
CN100417801C (zh) 2008-09-10
JP2009150402A (ja) 2009-07-09
IL145349A0 (en) 2002-06-30
AU6045800A (en) 2000-10-09
CA2364284C (fr) 2008-05-06
WO2000057048A3 (fr) 2001-01-18
WO2000057048A2 (fr) 2000-09-28
JP2009150401A (ja) 2009-07-09
US6220016B1 (en) 2001-04-24
DE60038012T2 (de) 2009-02-12
DE60038012D1 (de) 2008-03-27
EP1171705B1 (fr) 2008-02-13
IL164184A0 (en) 2005-12-18
RU2243403C2 (ru) 2004-12-27
EP1171705A4 (fr) 2005-01-12
CN1201076C (zh) 2005-05-11
US6269647B1 (en) 2001-08-07

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